CN100359823C - Apparatus and method for reusing satellite broadcast spectrum for terrestrially broadcast signals - Google Patents

Apparatus and method for reusing satellite broadcast spectrum for terrestrially broadcast signals Download PDF

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Publication number
CN100359823C
CN100359823C CNB971800235A CN97180023A CN100359823C CN 100359823 C CN100359823 C CN 100359823C CN B971800235 A CNB971800235 A CN B971800235A CN 97180023 A CN97180023 A CN 97180023A CN 100359823 C CN100359823 C CN 100359823C
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satellite
land
signal
antenna
frequency
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CN1238867A (en
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C·他因
S·他因
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BROADBAND INVESTMENTS Ltd
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Diversified Communication Engineering Inc
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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04HBROADCAST COMMUNICATION
    • H04H40/00Arrangements specially adapted for receiving broadcast information
    • H04H40/18Arrangements characterised by circuits or components specially adapted for receiving
    • H04H40/27Arrangements characterised by circuits or components specially adapted for receiving specially adapted for broadcast systems covered by groups H04H20/53 - H04H20/95
    • H04H40/90Arrangements characterised by circuits or components specially adapted for receiving specially adapted for broadcast systems covered by groups H04H20/53 - H04H20/95 specially adapted for satellite broadcast receiving
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/185Space-based or airborne stations; Stations for satellite systems
    • H04B7/18523Satellite systems for providing broadcast service to terrestrial stations, i.e. broadcast satellite service
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/185Space-based or airborne stations; Stations for satellite systems
    • H04B7/1853Satellite systems for providing telephony service to a mobile station, i.e. mobile satellite service
    • H04B7/18563Arrangements for interconnecting multiple systems
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N7/00Television systems
    • H04N7/20Adaptations for transmission via a GHz frequency band, e.g. via satellite
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04WWIRELESS COMMUNICATION NETWORKS
    • H04W4/00Services specially adapted for wireless communication networks; Facilities therefor
    • H04W4/06Selective distribution of broadcast services, e.g. multimedia broadcast multicast service [MBMS]; Services to user groups; One-way selective calling services
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04WWIRELESS COMMUNICATION NETWORKS
    • H04W84/00Network topologies
    • H04W84/02Hierarchically pre-organised networks, e.g. paging networks, cellular networks, WLAN [Wireless Local Area Network] or WLL [Wireless Local Loop]
    • H04W84/04Large scale networks; Deep hierarchical networks
    • H04W84/06Airborne or Satellite Networks

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Signal Processing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Multimedia (AREA)
  • Radio Relay Systems (AREA)
  • Two-Way Televisions, Distribution Of Moving Picture Or The Like (AREA)

Abstract

A first antenna (16) at a user location (14) receives signals at a first frequency where the signals are travelling only within a first directional reception range as measured from a centerline (28) of the first antenna (16). The first antenna (16) has its centerline (28) aligned to receive direct broadcast satellite signals transmitted from a satellite in geosynchronous orbit about the earth. A second antenna (18) at the user location (14) receives signals at the first frequency where the signals are travelling only within a second directional reception range as measured from a centerline (30) of the second antenna (18). The second antenna (18) is aligned to receive signals transmitted at the first frequency from a terrestrial transmitting location remote from the user location. A terrestrial transmitter transmits signals at the first frequency and directionally within a terrestrial azimuth range from the terrestrial transmitting location. The terrestrial transmitting location is located with respect to the user location such that the terrestrial transmitter (20) transmits in directions only outside of the directional reception range of the first antenna (16). The satellite (12) is positioned with respect to the user location (14) such that the satellite transmits directional in directions outside of the directional reception range of the second antenna (18).

Description

Terrestrially broadcast signals utilizes the apparatus and method of satellite broadcast spectrum again
Technical field
The present invention relates to play and receive the apparatus and method of the data that comprise TV signal and voice signal, more particularly, the present invention relates to the apparatus and method of land emission and direct broadcasting satellite emission are provided on shared frequency simultaneously.
Background of invention
At present, can received television signal from the satellite of geostationary orbit.TV signal can be transmitted into satellite from land transmitter, emission again from the satellite then, thus make the land receiver in the certain geographical receiving area in the satellite sight line can receive signal.Except TV signal, the data of other type also can be given the user by the satellites transmits in the geostationary orbit.
Direct broadcasting satellite service (DBS) refers to directly the satellite transmits for the TV signal of each family that has the particular suitable signal receiver or user's use.The committee of united telecommunication has specialized in the electromagnetic spectrum of 12.2GHz to 12.7GHz DBS broadcasting and has used.16 signal carriers are positioned at the DBS frequency spectrum, and each carrier wave is loaded with several television channels.Compress technique according to being used for these signals does not rant out, can provide hundreds of frequencies separately by DBS.Opposite with existing satellite system, the maximum of DBS system is benefited and is, only needs small-sized parabolic shape antenna to receive the DBS signal, and the aligning of reception antenna is not very crucial.In addition, the DBS system will provide high-quality reception on any point in the geographical receiving area of satellite, need not to spend such as the required this land transmission line of cable TV.
Present regulation requires the DBS satellite to be separated from each other at least 9 degree on the synchronous camber line of the earth.Therefore, the reception antenna of DBS signal must be limited to the orientation range received signal at positive and negative 9 degree of measuring from center of antenna.Received signal will cause the interference of the signal that different satellites are launched on same frequency in the scope wideer than satellite spacing.
The 5th, 483, No. 663 United States Patent (USP)s are meant to have the system that a kind of like this receiver is arranged, and wherein DBS receives in similar frequency band with land signal.Indicated system can realize with a kind of many antenna configurations or with a single movably antenna in the 5th, 483, No. 663 United States Patent (USP)s.In many antenna configurations, two independent antennas are sent to a shared propagation path with received signal and handle, seem they be receive by individual antenna and from the emission of single position.In the individual antenna configuration, antenna is movably between the another location of position that receives the DBS signal and the land signal of reception.
The advantage of the 5th, 483, No. 663 described systems of United States Patent (USP) is, no matter local initial spike is TV signal or other data, can receive simultaneously with the DBS signal and is used for the identical device that the DBS signal is handled is handled.Local initial spike can be loaded with local program, and it can receive with the DBS program of this country or this area.
Yet, the 5th, 483, in the system described in No. 663 United States Patent (USP)s, because therefore received signal, can not receive land on shared frequency and the DBS signal in combination in time or receive on the same antenna structure on the different location simultaneously.
Although DBS has its advantage, the 5th, 483, No. 663 there is its advantage in the described system of United States Patent (USP),, the DBS system has taken a part of electromagnetic spectrum, otherwise this part frequency spectrum can use for land signal emission.
Brief summary of the invention
The purpose of this invention is to provide provides land simultaneously with same frequency and transmits and satellite emission signal.The present invention includes a kind ofly provides land and apparatus and method satellite-signal simultaneously with shared frequency.
Utilization has the reception antenna of limited directional reception scope and launches land signal and can realize purpose of the present invention on the direction that is different from the satellite-signal transmit direction.The present invention needs two independent reception antennas, presents to two groups of decodings and demodulation process system, to utilize received signal.Two reception antennas all are suitable for receiving the only signal in the certain orientation scope.This scope is from the central line measurement of specific antenna.
In order not disturb between the signal that guarantees satellite and land emission, the land azimuth coverage interior orientation outside the azimuth coverage of the signal of being launched an artificial satellite by single satellite or multi-satellite is launched land signal.Land launch azimuth angular region is chosen such that to be that it does not comprise that satellite signal receiving antenna must point to any direction from any satellite received signal.In order to cover the zone of bigger local reception, a plurality of land transmitters are dispersed on the equitant zone, directional transmissions district, to guarantee clearly to receive land signal on each position in the required service district.
From following description to preferred embodiment, and take accompanying drawing into consideration, these and other purpose, advantage and feature of the present invention will be very clearly.
The accompanying drawing summary
Fig. 1 shows the schematic diagram of a plurality of satellites with respect to the position relation of single land transmitter and receiver or customer location.
Fig. 2 is the schematic diagram that receives satellite and the land reception antenna structure that transmits on shared frequency.
Fig. 3 is the schematic diagram that allows at the interval of managing several required land transmitters of reception on the zone significantly.
The description of preferred embodiment
Satellite and the land device that transmits of providing simultaneously on same frequency of the present invention is provided Fig. 1 and 2.As shown in Figure 1, in geostationary orbit, can adopt system with one or more satellites.Fig. 1 illustrates four satellite 12a, 12b, 12c and 12d that spatially separate on four different directions that depart from customer location 14.In geostationary orbit, every satellite is with respect to earth surface, and therefore the position with respect to user 14 is maintained fixed.First antenna 16 and second antenna 18 lay respectively on the customer location 14, go through below with reference to Fig. 2.
Among these satellites 12a-12d each is arranged in the geostationary orbit about ground ball center, is positioned on the particular longitude and latitude of earth surface top.Known as one of skill in the art, reception antenna can point to required satellite position with the specific azimuth and the angle of pitch, from the particular satellite received signal.
At present, longitude of locating of all direct broadcasting satellites in the visual line of sight of North America and latitude require reception antenna with the direction to the south from the North America towards satellite received signal.Although in order to describe Fig. 1 of the present invention four satellite 12a-12d are shown here, more or less satellite that spatially separates can be arranged in the visual line of sight of certain geographic area.At present, eight satellites are arranged in the visual line of sight of North America.Table 1 has been listed longitude station and the azimuth and the angle of pitch of every satellite, and reception antenna must point to this orientation from Texan Jane Austen position, receives the signal of every satellite.All azimuth directions and pitch orientation are measured with respect to antenna centerline, will discuss at Fig. 2 below.Term " azimuth " is meant with respect to the reference direction such as positive north, is taken as the direction of 0 degree usually, and " angle of pitch " is meant the angle that antenna centerline makes progress in level.
Table 1
The satellite longitude The azimuth The angle of pitch
61.5 124.5 37.3
101 186.4 54.6
110 203.3 52.3
119 217.7 47.8
148 247.3 25.7
157 253.3 17.9
166 258.8 10.1
175 263.5 2.3
The DBS satellite is all launched unlike signal on identical frequency band.The committee of united telecommunication has broadcasted to DBS and has reserved 12.2GHz to 12.7GHz electromagnetic spectrum.In order to guarantee that two signals between the adjacent satellite do not disturb, must satisfy two conditions.At first, reception antenna must be limited to only received signal in certain range of receiving of antenna centerline.Secondly, satellite must separate in the space on the synchronous camber line of the earth, thereby can position reception antenna, makes and has only a satellite in emission in the directional reception scope of antenna.
According to present regulation, each DBS satellite must separate at least 9 degree on the synchronous camber line of the earth.Therefore, when when antenna centerline is measured, every DBS reception antenna must have plus or minus 9 degree or littler directional reception scope or apertures.Although present regulation requires to be not less than at interval 9 degree,, the invention is not restricted to this and separate angle.Yet according to the present invention, effective range of receiving of each first antenna or satellite earth antenna must be less than or equal to minimum satellite vehicle angle at interval.
Fig. 1 also illustrates land transmitter 20 can be to launch on one or more frequencies identical with one of DBS satellite institute emission spectrum.Land transmitter 20 is in certain transmitting boundary T interior orientation emission.Transmitting boundary T shown in Fig. 1 is 180 degree.Certainly, transmitting boundary can be greater than or less than this numeral.
Fig. 2 is illustrated in the antenna structure of the present invention 22 that is positioned among Fig. 1 on the customer location 14 by way of example.First antenna 16 is designed to receive the direct broadcasting satellite signal.First antenna 16 comprises the parabolic feed horn assembly 26 of collecting antenna 24 and receiving the signal that is collected antenna-reflected and concentrates.One of skill in the art will be appreciated that feed horn 26 comprises the probe of searching antenna receiving signal, and is not shown among Fig. 2.This probe feeds signals to the signal handling equipment of information extraction from received signal.This signal handling equipment is well-known prior art, does not constitute a part of the present invention.In addition, relevant professional will be appreciated that, can adopt the alternative feed horn assembly 26 of collecting the signal of polished object surface antenna 24 reflections of assembly of numerous species type.
First antenna 16 comprises antenna centerline 28.Represented as the frequency with received signal, first antenna 16 has the maximum directional reception scope d that measures from antenna centerline 28 MaxThe signal of propagating on direction outside this range of receiving of antenna centerline 28 or the aperture can not be received by first antenna 16.
Still with reference to figure 2, the antenna structure 22 that is positioned on the customer location 14 further comprises the land second independent antenna 18 that transmits of reception.Second antenna 18 is as shown in the feed horn type antenna, yet the professional who is familiar with present technique will be appreciated that second antenna can comprise circular waveguide antenna, plate aerial, slot antenna, dipole antenna or multistage dipole antenna.No matter antenna type how, antenna will comprise that one is searched the antenna received signal and the appropriate signals that this signal is fed to the appropriate signals treatment facility is searched assembly.This treatment facility is what to separate with the treatment facility of handling first antenna, 16 received signals.In addition, although second antenna 18 shown in the figure equally is connected to same structure with first antenna 16,, first and second antennas can separate fully.In any situation, second antenna 18 is preferably around vertical axis and rotates, and shown in B among Fig. 2, making antenna direction is the optimum reception that transmits to land.
The same with first antenna 16, second antenna 18 comprises center line 30, the directional reception scope r that only can receive in antenna centerline 30 MaxThe interior signal of propagating.The signal of propagating on the direction outside this range of receiving can not be received by second antenna 18.
With reference to figure 1, first antenna 16 of the present invention is directed to reception from one of satellite, for example the signal of satellite 12d again.For from satellite 12d received signal best, must make first antenna 16 be oriented in the certain azimuth and the angle of pitch, for example can be respectively that 247.3 degree and 25.7 are spent.The center line 30 of second antenna 18 is often referred to the land transmitting site to land transmitter 20, is level substantially.Ignore the pitching angular difference between each first antenna 16 and second antenna 18, the angle of cut between the center line 28 and 30 of two antennas is about 67.7 degree in this example.
In orientation shown in Figure 1, first antenna 16 can not receive the signal from land transmitter 20.Its reason be the phasing signal launched from land transmitter 20 all the direction outside the range of receiving of first antenna 16 propagate.Equally, satellite 12d with respect to the direction of customer location 14 emission outside the range of receiving of second antenna 18.Therefore, second antenna 18 can not receive the signal that satellite 12d is launched.In addition, in this example, second antenna can not receive any any signal of being launched among the satellite 12a-12d.Therefore, in the orientation of as shown in Figure 1 first antenna 16 and second antenna 18 and position with satellite 12a-12d and land transmitter 20, land transmitter can be launched on the frequency identical with the frequency of satellite emission signal, and the signal that is received on two antennas is without any interference.
The personnel that are familiar with prior art will be appreciated that, the angle of pitch of first antenna 16 can be enough high with respect to horizontal line, so that second antenna 18 can aim at along the azimuth identical with first antenna, and by two antennas between the signal that is received on the same frequency without any interference.Yet, exist many to have the place of the satellite of the different orientations and the angle of pitch with respect to customer location 14, first antenna 16 and second antenna 18 can be positioned on as shown in Figure 1 the different azimuth, with anti-tampering.
With reference to figure 3, need provide intensity to be enough to received signal on big zone with a plurality of land transmitters 32.Each transmitter 32 among Fig. 3 is launched at about 180 azimuth coverage A and the longest effective receiving range R interior orientation.Adopt this transmitter at interval and transmitting range, can receive signal on any position in the G of geographic area from land transmitter.Although for the azimuth coverage that there is shown 180 for example,, within the scope of the invention, land emission can fix on other scope.
The method according to this invention comprises the satellite-signal that receives first frequency with first antenna 16.First antenna 16 is suitable for receiving only at the signal in the first directional reception scope of antenna centerline 28.This method also comprises in the scope outside first antenna, the 16 directional reception scopes with first frequency directional transmissions signal.The signal of being launched by land transmitter is received by second antenna of customer location 14.Second antenna only also is suitable for receiving with respect to the signal in the directional reception scope of antenna centerline 30.
Directional receiving antenna 16 and this combination of 18 and directed land emission allow with satellite, particularly the frequency that the DBS frequency of utilization is identical is carried out land emission, and does not disturb between two kinds of emissions.This just allows a DBS frequency spectrum, and perhaps other satellite frequency spectrum is by the utilization again of land emission institute.Land emission can be TV signal or any other data, comprises the data of Internet traffic, speech data, other video or other any kind.
Preferred embodiment described above attempts to illustrate principle of the present invention, rather than limits the scope of the invention.Only otherwise deviate from the scope of following claim, the personnel that are familiar with prior art can make various other embodiment and to the improvement of these preferred embodiments.

Claims (35)

1. one kind provides transmit device with the direct broadcasting satellite signal that satellite is launched on being arranged in geostationary orbit first satellite position of land on the shared frequency simultaneously, it is characterized in that described device comprises:
(a) be positioned at first antenna on the customer location, only receive at the signal in the first directional reception scope of the central line measurement of first antenna with first frequency, the center line that makes first antenna is in alignment with receiving the direct broadcasting satellite signal that this satellite is launched;
(b) be positioned at second antenna on the customer location, only receive at the signal in the second directional reception scope of the central line measurement of second antenna with first frequency, make second antenna alignment in the signal that receives from being launched with first frequency away from the land transmitting site of customer location, the direct broadcasting satellite signal is to launch on the direction outside the second directional reception scope; With
(c) land transmitter, transmit with first frequency and at the land bearing range interior orientation that departs from land transmitter site, land transmitter site is to locate like this with respect to customer location, and promptly land transmitter is only launched on the direction outside the directional reception scope of first antenna.
2. device as claimed in claim 1, wherein, the direct broadcasting satellite signal is with many additional satellites transmits of first frequency from geostationary orbit, and wherein, land transmitter is located like this with respect to customer location, make land transmitter only on the direction beyond the directional reception scope of first antenna, launch to customer location, first antenna any locational be oriented to it can receive from first satellite position in satellite emission or from a plurality of additional satellites in the emission of any one satellite.
3. device as claimed in claim 2 is characterized in that further comprising:
(a) a plurality of land transmitters, each transmitter is launched from different land transmitting sites, and each transmitter is launched with common substantially azimuth coverage.
4. device as claimed in claim 1 is characterized in that: described first frequency is in the scope of 12.2GHz to 12.7GHz.
5. device as claimed in claim 1 is characterized in that: described first frequency is higher than 12.2GHz.
6. device as claimed in claim 1 is characterized in that: described second antenna is selected from one group of antenna being made up of circular waveguide antenna, feed horn antenna, plate aerial, slot antenna, dipole antenna or multistage dipole antenna.
7. device as claimed in claim 1 is characterized in that: the directional reception scope of first antenna is about 9 degree.
8. one kind provides land on the shared frequency to transmit and method from the direct broadcasting satellite signal of satellites transmits simultaneously, and satellite described here is arranged in first satellite position of geostationary orbit, it is characterized in that described method comprises step:
(a) on customer location, receive the direct broadcasting satellite signal of first frequency with first antenna, first antenna only is suitable for receiving the signal at the first frequency in the first directional reception scope of the central line measurement of first antenna;
(b) from land transmitter with first frequency and the land signal of emission in the bearing range by land, land azimuth coverage is outside the directional reception scope of first antenna, first antenna is located in the direct broadcasting satellite signal that receives satellite; With
(c) on customer location away from land transmitter, receive land signal with second antenna, second antenna only is suitable for receiving the signal at the first frequency in the second directional reception scope of the central line measurement of second antenna, making second antenna alignment, is not to launch in the directional reception scope of second antenna thereby make the direct broadcasting satellite signal of satellites transmits.
9. method as claimed in claim 8 is characterized in that further comprising step:
(a) from a plurality of additional land transmitters with first frequency and by land azimuth coverage launch land signal, it is a plurality of that to add land transmitters spatially spaced apart so that continuous basically land service area to be provided.
10. method as claimed in claim 8 is characterized in that: described first frequency is in the scope of 12.2GHz to 12.7GHz.
11. method as claimed in claim 8 is characterized in that: described first frequency is higher than 12.2GHz.
12. method as claimed in claim 8 is characterized in that: the orientation range of first antenna is for departing from about 9 degree of this antenna centerline.
13. land signal and device of launching simultaneously on the shared frequency from the satellite-signal of satellites transmits, described satellite with first frequency to the customer location signal of launching an artificial satellite, only be used for it is characterized in that described device comprises about the reception in the satellite orientation range of receiving of this customer location:
(a) with the directed land transmitter of first frequency at the land signal of emission in the limited azimuth coverage of land transmitter site, land transmitter is to locate like this with respect to customer location, and promptly land transmitter is launched to customer location along the route outside the satellite orientation range of receiving.
14. device as claimed in claim 13, it is characterized in that: satellite-signal is that the multi-satellite from geostationary orbit is launched, the angle that every each satellite of satellite and other separates on the synchronous camber line of the earth is greater than 1/2nd of satellite orientation range of receiving, and these satellites only in about the combination satellite signal transmitting boundary of customer location together to the customer location signal of launching an artificial satellite, here:
(a) land transmitter only on the direction outside the combination satellite signal transmitting boundary and with combination satellite signal firing zone boundary outside satellite orientation range of receiving 1/2nd angle same launch.
15. device as claimed in claim 14 is characterized in that further comprising:
(a) a plurality of land directional transmitters, each transmitter is launched from different land transmitting sites, and each transmitter carries out directional transmissions at limited azimuth coverage.
16. device as claimed in claim 13 is characterized in that: described first frequency is in the scope of 12.2GHz to 12.7GHz.
17. device as claimed in claim 13 is characterized in that: described first frequency is higher than 12.2GHz.
18. device as claimed in claim 13 is characterized in that: the satellite orientation range of receiving is about 18 degree.
19. one kind provides the land signal and method from the satellite-signal of satellites transmits on the shared frequency simultaneously, satellite described here is launched along the satellites transmits axle that extends to land customer location from satellite with first frequency, it is characterized in that described method comprises step:
(a) in limited azimuth coverage, launch land signal with first frequency from land transmitter, land transmitter is to locate like this with respect to customer location, promptly along launching to customer location about the transmission route outside the satellite orientation range of receiving of customer location, wherein the satellite orientation range of receiving comprises the center limited orientation range on the satellites transmits axle basically.
20. method as claimed in claim 19 is characterized in that further comprising step:
(a) on the different positions from a plurality of land transmitters with first frequency and in limited azimuth coverage the land signal of emission.
21. method as claimed in claim 19 is characterized in that: described first frequency is in the scope of 12.2GHz to 12.7GHz.
22. method as claimed in claim 19 is characterized in that: described first frequency is higher than 12.2GHz.
23. method as claimed in claim 19 is characterized in that: the satellite orientation range of receiving is about 18 degree.
24. device of being convenient to the land use that transmits, described land transmitting is to launch simultaneously on shared frequency Yu from the satellite-signal of satellites transmits, this satellite along the satellites transmits axle with first frequency to the land customer location signal of launching an artificial satellite, it is characterized in that described device comprises:
(a) be used for launching to customer location the land transmitter of land signal with first frequency, this land transmitter is to locate like this with respect to customer location, promptly along launching to customer location about the route outside the satellite orientation range of receiving of customer location, wherein the satellite orientation range of receiving comprises the center limited orientation range on the emission shaft of position basically; And
(b) the land reception antenna on the customer location, be used to receive only at signal about the first frequency in the land directional reception scope of land antenna centerline, land antenna is aimed at, to receive signal with the first frequency emission from land transmitter site, with land antenna is aimed at, thereby make the satellites transmits axle by land outside the directional reception scope.
25. device as claimed in claim 24, wherein, described satellite-signal is that the multi-satellite from geostationary orbit is launched, the angle that every each satellite of satellite and other separates on the synchronous camber line of the earth is greater than the angle of satellite orientation range of receiving 1/2nd, and these satellites only in about the combination satellite signal transmitting boundary of customer location together to the customer location signal of launching an artificial satellite, here:
(a) land transmitter only on the direction outside the combination satellite signal transmitting boundary and with combination satellite signal firing zone boundary outside satellite orientation range of receiving 1/2nd angle same launch.
26. device as claimed in claim 25 is characterized in that further comprising:
(a) a plurality of land transmitters, each transmitter is launched from different land transmitting sites, and each transmitter carries out directional transmissions at limited azimuth coverage.
27. device as claimed in claim 24 is characterized in that: described first frequency is in the scope of 12.2GHz to 12.7GHz.
28. device as claimed in claim 24 is characterized in that: described first frequency is higher than 12.2GHz.
29. device as claimed in claim 24 is characterized in that: the satellite orientation range of receiving is about 18 degree.
30. land signal and device of launching simultaneously on the shared frequency from the satellite-signal of satellites transmits, described satellite with first frequency to the customer location signal of launching an artificial satellite, only be used for it is characterized in that described device comprises about the reception in the satellite orientation range of receiving of this customer location:
(a) be used for first frequency from one fixedly onshore location launch the directed land transmitter of land signal, be somebody's turn to do the fixedly geometrical relationship of fixedly onshore location formation and customer location and satellite, land transmitter is to locate like this with respect to customer location, and promptly land transmitter is along launching to customer location about the route outside the satellite orientation range of receiving of customer location.
31. device as claimed in claim 30, it is characterized in that: satellite-signal is that the multi-satellite from geostationary orbit is launched, the angle that every each satellite of satellite and other separates on the synchronous camber line of the earth is greater than 1/2nd of satellite orientation range of receiving, and these satellites only in about the combination satellite signal transmitting boundary of customer location together to the customer location signal of launching an artificial satellite, here:
(a) land transmitter only on the direction outside the combination satellite signal transmitting boundary and with combination satellite signal firing zone boundary outside satellite orientation range of receiving 1/2nd angle same launch.
32. device as claimed in claim 31 is characterized in that further comprising:
(a) a plurality of land transmitters, each transmitter is launched from different fixing land transmitting sites, the fixedly geometrical relationship of this position formation and satellite and customer location.
33. device as claimed in claim 30 is characterized in that: described first frequency is in the scope of 12.2GHz to 12.7GHz.
34. device as claimed in claim 30 is characterized in that: described first frequency is higher than 12.2GHz.
35. device as claimed in claim 30 is characterized in that: the satellite orientation range of receiving is about 18 degree.
CNB971800235A 1996-10-11 1997-10-09 Apparatus and method for reusing satellite broadcast spectrum for terrestrially broadcast signals Expired - Fee Related CN100359823C (en)

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US08/731,244 US5761605A (en) 1996-10-11 1996-10-11 Apparatus and method for reusing satellite broadcast spectrum for terrestrially broadcast signals
US08/731,244 1996-10-11

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CN1238867A CN1238867A (en) 1999-12-15
CN100359823C true CN100359823C (en) 2008-01-02

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EP (1) EP0934636B1 (en)
JP (1) JP2001514810A (en)
KR (1) KR100415416B1 (en)
CN (1) CN100359823C (en)
AT (1) ATE286328T1 (en)
AU (1) AU721537B2 (en)
BR (1) BR9712232A (en)
CA (1) CA2268393C (en)
DE (1) DE69732128D1 (en)
HK (1) HK1023462A1 (en)
NZ (1) NZ335562A (en)
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US7853197B2 (en) 2010-12-14
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US20060079176A1 (en) 2006-04-13
AU4750697A (en) 1998-05-11
US20010019942A1 (en) 2001-09-06
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US5761605A (en) 1998-06-02
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US6519446B2 (en) 2003-02-11
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US6169878B1 (en) 2001-01-02
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RU2196386C2 (en) 2003-01-10
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